*HEADING
 PLANE STRESS PLASTICITY TEST, BIAXIAL LOAD [SC8R]
*NODE
*NGEN,NSET=NX
*NGEN,NSET=NY
*NGEN
*NSET,NSET=FIXR
*ELEMENT,TYPE=SC8R,ELSET=EALL
*SHELL SECTION,MATERIAL=A1,ELSET=EALL
 .001,
*MATERIAL,NAME=A1
*ELASTIC
 30.E6,0.3
*PLASTIC,HARDENING=KINEMATIC
 3.E4,
 1.54E6,0.95
*BOUNDARY
 NX,2
 NY,1
*EQUATION
*EQUATION
*AMPLITUDE,NAME=P2,INPUT=PLATE2.AMP,VALUE=ABSOLUTE,TIME=TOTAL TIME
*AMPLITUDE,NAME=P3,INPUT=PLATE3.AMP,VALUE=ABSOLUTE,TIME=TOTAL TIME
*RESTART,WRITE,FREQUENCY=5
*STEP,INC=84
  BIAXIAL LOAD
*STATIC,DIRECT
 .01,.84
*PRINT,RESIDUAL=NO
*CLOAD,AMPLITUDE=P2
 15,1,1.
*CLOAD,AMPLITUDE=P3
 23,2,1.
*EL PRINT,SUMMARY=NO,POSITION=CENTROIDAL
S ,E
PE,
*EL FILE,ELSET=EALL,POSITION=CENTROIDAL
S,
PE,PEP
*OUTPUT, HISTORY
*ELEMENT OUTPUT, ELSET=EALL
 S,
 E,
 PE,
*NODE PRINT,SUMMARY=NO
U1,U2,RF1,RF2,CF1,CF2
*END STEP